Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data

Author:	Sivells, James C.
Year:	1950
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1090
Link:	https://digital.library.unt.edu/ark:/67531/metadc60450/